发明名称 |
Aircraft body member, more particularly for supersonic aircraft, made from a long-living, damage tolerant aluminium alloy with good stress corrosion resistance |
摘要 |
<p>An aircraft component is made of an Al alloy containing 2.00-3.00 wt.% Cu, 1.40-1.90 wt.% Mg, 0.20-0.70 wt.% Mn, 0-0.30 wt.% Fe, 0-0.30 wt.% Ni, 0-0.15 wt.% Ti, at least 0.05 wt.% Si and 0-1.10% Ag, where 0.40 ≤ Si + 0.4 Ag ≤ 0.60 and Si + Ag + 1.1 Mg ≤ 2.6. One alloy exemplified contains 0.40-0.60% Si and no Ag, and another contains 0.20-0.40% Si and 0.40-0.60% Ag.</p> |
申请公布号 |
EP0756016(A1) |
申请公布日期 |
1997.01.29 |
申请号 |
EP19960401680 |
申请日期 |
1996.07.26 |
申请人 |
AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE |
发明人 |
PONS, GILLES;BARBAUX, YANN PHILIPPE |
分类号 |
C22C21/12;C22C21/16;(IPC1-7):C22C21/16 |
主分类号 |
C22C21/12 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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